Date: July 21st 2008

ISS TRAJECTORY DATA

Lift off time (UTC) : N/A Area (sq ft) : 6135 43 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 71 3 Monthly MSFC 50% earth geomagnetic index (Kp) : 2 07 ET - UTC (sec) : 65 18 UT1 - UTC (sec) : 0 00

Maneuvers contained within the current ephemeris are as follows:

IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP


205/16:18:03 264 -11 0 11 8 11 8
N/A 1 7 -0 0 191 9
000/00:22:06 528 -4 0 -0 1 186 9

Coasting Arc #1 (Orbit 3315)
---------------------------------------

Vector Time (GMT): 2008/198/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -124583
05                 A    =         6720621
20  meter
 Y    =       -5059059
72  meter          E    =           
0013193
 Z    =        4408940
87                 I    =           51
39976
 XDOT =       6448
911046                 Wp   =           63
49219
 YDOT =       2687
421426  meter/sec      RA   =          224
52228  deg
 ZDOT =       3264
224424                 TA   =          353
70447
                                          MA   =          353
72103
                                          Ha   =            191
130  n
mi
                                          Hp   =            180
225

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -408737
05                 X    =          -89420
14
 Y    =      -16597964
96  feet           Y    =        -5060257
10  meter
 Z    =       14465029
11                 Z    =         4408420
12
 XDOT =      21157
844638                 XDOT =        6402
523772
 YDOT =       8816
999428  feet/sec       YDOT =        2759
276869  meter/sec
 ZDOT =      10709
397716                 ZDOT =        3295
440667

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -12677170
67                 X    =        -3864001
62
 Y    =       10724761
26  feet           Y    =         3268907
23  meter
 Z    =       14462552
11                 Z    =         4408185
88
 XDOT =      -5463
966919                 XDOT =       -1665
417117
 YDOT =     -21070
640017  feet/sec       YDOT =       -6422
331077  meter/sec
 ZDOT =      10830
000727                 ZDOT =        3300
984222


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08198
59386474  
00020000  00000-0  20000-3 0  9001
2 25544  51
6381 225
1586 0009792  18
9078 341
2447 15
75079536 33161


Satellite: ISS
Catalog Number: 25544
Epoch time:      08198
59386474   =   yrday
fracday
Element set:     900
Inclination:       51
6381  deg
RA of node:       225
1586  deg
Eccentricity:     
0009792     
Arg of perigee:    18
9078  deg
Mean anomaly:     341
2447  deg
Mean motion:   15
75079536  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3316
Checksum:              324


Coasting Arc #2 (Orbit 3330)
---------------------------------------

Vector Time (GMT): 2008/199/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -5835757
08                 A    =         6726130
75  meter
 Y    =       -2172615
08  meter          E    =           
0014520
 Z    =       -2530161
68                 I    =           51
44121
 XDOT =       -193
680574                 Wp   =           32
73040
 YDOT =      -5602
590918  meter/sec      RA   =          219
31774  deg
 ZDOT =       5283
684037                 TA   =          298
49352
                                          MA   =          298
63967
                                          Ha   =            191
104  n
mi
                                          Hp   =            179
950

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -19146184
65                 X    =        -5798737
97
 Y    =       -7128002
24  feet           Y    =        -2237666
43  meter
 Z    =       -8301055
39                 Z    =        -2558421
79
 XDOT =       -635
434953                 XDOT =        -156
683865
 YDOT =     -18381
203798  feet/sec       YDOT =       -5604
550850  meter/sec
 ZDOT =      17334
921381                 ZDOT =        5282
832015

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6654971
20                 X    =         2028435
22
 Y    =       19268412
72  feet           Y    =         5873012
20  meter
 Z    =       -8410229
04                 Z    =        -2563437
81
 XDOT =     -12306
612516                 XDOT =       -3751
055495
 YDOT =      11778
242239  feet/sec       YDOT =        3590
008234  meter/sec
 ZDOT =      17331
110230                 ZDOT =        5282
522398


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08199
54554609  
00020000  00000-0  20000-3 0  9015
2 25544  51
6385 220
2641 0009800  22
5396 337
6196 15
75116883 33311


Satellite: ISS
Catalog Number: 25544
Epoch time:      08199
54554609   =   yrday
fracday
Element set:     901
Inclination:       51
6385  deg
RA of node:       220
2641  deg
Eccentricity:     
0009800     
Arg of perigee:    22
5396  deg
Mean anomaly:     337
6196  deg
Mean motion:   15
75116883  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3331
Checksum:              298


Coasting Arc #3 (Orbit 3346)
---------------------------------------

Vector Time (GMT): 2008/200/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         153106
27                 A    =         6719068
51  meter
 Y    =        4724224
30  meter          E    =           
0019819
 Z    =       -4793508
30                 I    =           51
43930
 XDOT =      -6902
934807                 Wp   =           51
32927
 YDOT =      -2299
551074  meter/sec      RA   =          214
20058  deg
 ZDOT =      -2481
515226                 TA   =          194
26073
                                          MA   =          194
31675
                                          Ha   =            191
282  n
mi
                                          Hp   =            179
846

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =         502317
17                 X    =          123553
40
 Y    =       15499423
55  feet           Y    =         4725771
96  meter
 Z    =      -15726733
28                 Z    =        -4792835
54
 XDOT =     -22647
423909                 XDOT =       -6864
653309
 YDOT =      -7544
458904  feet/sec       YDOT =       -2376
529206  meter/sec
 ZDOT =      -8141
454155                 ZDOT =       -2514
956421

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11400033
40                 X    =         3474730
18
 Y    =      -10517576
72  feet           Y    =        -3205757
38  meter
 Z    =      -15723689
48                 Z    =        -4792580
55
 XDOT =       8176
560265                 XDOT =        2492
215569
 YDOT =      21253
036730  feet/sec       YDOT =        6477
925595  meter/sec
 ZDOT =      -8270
635739                 ZDOT =       -2520
889773


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08200
56066516  
00020000  00000-0  20000-3 0  9026
2 25544  51
6372 215
0413 0009819  25
7736 334
3915 15
75107002 33472


Satellite: ISS
Catalog Number: 25544
Epoch time:      08200
56066516   =   yrday
fracday
Element set:     902
Inclination:       51
6372  deg
RA of node:       215
0413  deg
Eccentricity:     
0009819     
Arg of perigee:    25
7736  deg
Mean anomaly:     334
3915  deg
Mean motion:   15
75107002  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3347
Checksum:              270


Coasting Arc #4 (Orbit 3362)
---------------------------------------

Vector Time (GMT): 2008/201/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6221522
19                 A    =         6727457
83  meter
 Y    =        1820110
90  meter          E    =           
0017992
 Z    =        1791160
97                 I    =           51
49279
 XDOT =        118
603771                 Wp   =           80
72065
 YDOT =       5216
912783  meter/sec      RA   =          209
00700  deg
 ZDOT =      -5662
088225                 TA   =           79
38104
                                          MA   =           79
17845
                                          Ha   =            191
326  n
mi
                                          Hp   =            179
584

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       20411818
20                 X    =         6192006
07
 Y    =        5971492
45  feet           Y    =         1889518
25  meter
 Z    =        5876512
38                 Z    =         1821313
06
 XDOT =        389
119985                 XDOT =          87
763432
 YDOT =      17115
855588  feet/sec       YDOT =        5218
067431  meter/sec
 ZDOT =     -18576
404937                 ZDOT =       -5661
586242

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -9027772
45                 X    =        -2751665
04
 Y    =      -19220248
89  feet           Y    =        -5858331
86  meter
 Z    =        5992979
13                 Z    =         1826660
04
 XDOT =      11090
848923                 XDOT =        3380
490752
 YDOT =     -11052
116108  feet/sec       YDOT =       -3368
684990  meter/sec
 ZDOT =     -18573
965373                 ZDOT =       -5661
344646


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08201
57577492  
00020000  00000-0  20000-3 0  9039
2 25544  51
6368 209
8187 0009990  28
9833 331
1883 15
75150508 33635


Satellite: ISS
Catalog Number: 25544
Epoch time:      08201
57577492   =   yrday
fracday
Element set:     903
Inclination:       51
6368  deg
RA of node:       209
8187  deg
Eccentricity:     
0009990     
Arg of perigee:    28
9833  deg
Mean anomaly:     331
1883  deg
Mean motion:   15
75150508  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3363
Checksum:              316


Coasting Arc #5 (Orbit 3378)
---------------------------------------

Vector Time (GMT): 2008/202/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         -33250
97                 A    =         6717789
31  meter
 Y    =       -4414023
06  meter          E    =           
0010900
 Z    =        5054545
88                 I    =           51
48576
 XDOT =       7313
833912                 Wp   =           60
62998
 YDOT =       1814
826250  meter/sec      RA   =          203
88261  deg
 ZDOT =       1635
592900                 TA   =           13
65607
                                          MA   =           13
62661
                                          Ha   =            191
392  n
mi
                                          Hp   =            179
551

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -109091
12                 X    =           -8443
76
 Y    =      -14481702
94  feet           Y    =        -4414256
76  meter
 Z    =       16583155
78                 Z    =         5054444
10
 XDOT =      23995
518083                 XDOT =        7285
051406
 YDOT =       5954
154363  feet/sec       YDOT =        1896
452621  meter/sec
 ZDOT =       5366
118438                 ZDOT =        1671
053084

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -10543133
56                 X    =        -3213547
11
 Y    =        9929818
75  feet           Y    =         3026608
76  meter
 Z    =       16582331
29                 Z    =         5054294
58
 XDOT =     -11067
761502                 XDOT =       -3373
453706
 YDOT =     -20926
813786  feet/sec       YDOT =       -6378
492842  meter/sec
 ZDOT =       5503
072163                 ZDOT =        1677
336395


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08202
59087696  
00020000  00000-0  20000-3 0  9045
2 25544  51
6364 204
5964 0009919  32
4795 327
6978 15
75133824 33798


Satellite: ISS
Catalog Number: 25544
Epoch time:      08202
59087696   =   yrday
fracday
Element set:     904
Inclination:       51
6364  deg
RA of node:       204
5964  deg
Eccentricity:     
0009919     
Arg of perigee:    32
4795  deg
Mean anomaly:     327
6978  deg
Mean motion:   15
75133824  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3379
Checksum:              335


Coasting Arc #6 (Orbit 3393)
---------------------------------------

Vector Time (GMT): 2008/203/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6504245
65                 A    =         6728321
38  meter
 Y    =       -1318521
44  meter          E    =           
0019523
 Z    =       -1054284
12                 I    =           51
54931
 XDOT =         54
479348                 Wp   =           37
87398
 YDOT =      -4940
081336  meter/sec      RA   =          198
70615  deg
 ZDOT =       5914
873598                 TA   =          310
56932
                                          MA   =          310
73910
                                          Ha   =            191
384  n
mi
                                          Hp   =            179
296

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21339388
62                 X    =        -6483896
90
 Y    =       -4325857
75  feet           Y    =        -1391141
78  meter
 Z    =       -3458937
41                 Z    =        -1085831
88
 XDOT =        178
738018                 XDOT =          80
983201
 YDOT =     -16207
615933  feet/sec       YDOT =       -4939
324465  meter/sec
 ZDOT =      19405
753274                 ZDOT =        5915
202181

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       11525549
97                 X    =         3512987
63
 Y    =       18449570
06  feet           Y    =         5623428
95  meter
 Z    =       -3580762
84                 Z    =        -1091416
51
 XDOT =     -10464
987224                 XDOT =       -3189
728106
 YDOT =      10259
280549  feet/sec       YDOT =        3127
028711  meter/sec
 ZDOT =      19406
531590                 ZDOT =        5915
110829


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08203
54252626  
00020000  00000-0  20000-3 0  9059
2 25544  51
6366 199
7013 0009937  37
0948 323
0901 15
75172580 33946


Satellite: ISS
Catalog Number: 25544
Epoch time:      08203
54252626   =   yrday
fracday
Element set:     905
Inclination:       51
6366  deg
RA of node:       199
7013  deg
Eccentricity:     
0009937     
Arg of perigee:    37
0948  deg
Mean anomaly:     323
0901  deg
Mean motion:   15
75172580  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3394
Checksum:              297


Coasting Arc #7 (Orbit 3409)
---------------------------------------

Vector Time (GMT): 2008/204/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        -174903
80                 A    =         6717028
84  meter
 Y    =        4232757
00  meter          E    =           
0022985
 Z    =       -5231728
87                 I    =           51
53951
 XDOT =      -7552
750853                 Wp   =           66
75522
 YDOT =      -1224
909493  meter/sec      RA   =          193
57112  deg
 ZDOT =       -732
156375                 TA   =          196
22078
                                          MA   =          196
29448
                                          Ha   =            191
539  n
mi
                                          Hp   =            179
192

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        -573831
37                 X    =         -196807
72
 Y    =       13886998
03  feet           Y    =         4230679
04  meter
 Z    =      -17164464
80                 Z    =        -5232631
43
 XDOT =     -24779
366316                 XDOT =       -7534
935750
 YDOT =      -4018
731933  feet/sec       YDOT =       -1309
269027  meter/sec
 ZDOT =      -2402
087844                 ZDOT =        -768
803958

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       10246685
91                 X    =         3123189
87
 Y    =       -9385008
98  feet           Y    =        -2860550
74  meter
 Z    =      -17167524
07                 Z    =        -5232661
34
 XDOT =      13789
203347                 XDOT =        4202
949180
 YDOT =      19746
291321  feet/sec       YDOT =        6018
669595  meter/sec
 ZDOT =      -2543
587130                 ZDOT =        -775
285357


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08204
55761052  
00020000  00000-0  20000-3 0  9060
2 25544  51
6370 194
4782 0009987  39
8836 320
3060 15
75152786 34108


Satellite: ISS
Catalog Number: 25544
Epoch time:      08204
55761052   =   yrday
fracday
Element set:     906
Inclination:       51
6370  deg
RA of node:       194
4782  deg
Eccentricity:     
0009987     
Arg of perigee:    39
8836  deg
Mean anomaly:     320
3060  deg
Mean motion:   15
75152786  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3410
Checksum:              300


Coasting Arc #8 (Orbit 3425)
---------------------------------------

Vector Time (GMT): 2008/205/12:58:12
196
Vector Time (MET): N/A
Weight (LBS)     : 661904
9

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6674221
05                 A    =         6728755
69  meter
 Y    =         817390
13  meter          E    =           
0016299
 Z    =         211910
75                 I    =           51
60887
 XDOT =       -380
497240                 Wp   =           94
56837
 YDOT =       4772
271303  meter/sec      RA   =          188
41309  deg
 ZDOT =      -6028
470383                 TA   =           83
12836
                                          MA   =           82
94296
                                          Ha   =            191
562  n
mi
                                          Hp   =            179
028

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21897050
68                 X    =         6663555
40
 Y    =        2681726
15  feet           Y    =          891965
45  meter
 Z    =         695245
24                 Z    =          244307
98
 XDOT =      -1248
350525                 XDOT =        -404
548295
 YDOT =      15657
058081  feet/sec       YDOT =        4767
882307  meter/sec
 ZDOT =     -19778
446139                 ZDOT =       -6030
376911

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -13715631
51                 X    =        -4180524
48
 Y    =      -17273227
40  feet           Y    =        -5264879
71  meter
 Z    =         820315
34                 Z    =          250032
12
 XDOT =      10536
148926                 XDOT =        3211
418193
 YDOT =      -9357
951090  feet/sec       YDOT =       -2852
303492  meter/sec
 ZDOT =     -19785
323195                 ZDOT =       -6030
566510


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08205
57268495  
00020000  00000-0  20000-3 0  9077
2 25544  51
6375 189
2557 0010072  42
8977 317
2971 15
75192884 34268


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
57268495   =   yrday
fracday
Element set:     907
Inclination:       51
6375  deg
RA of node:       189
2557  deg
Eccentricity:     
0010072     
Arg of perigee:    42
8977  deg
Mean anomaly:     317
2971  deg
Mean motion:   15
75192884  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3426
Checksum:              327


Coasting Arc #9 (Orbit 3427)
---------------------------------------

Vector Time (GMT): 2008/205/16:29:06
528
Vector Time (MET): N/A
Weight (LBS)     : 660953
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -2643948
60                 A    =         6725645
11  meter
 Y    =        3648345
18  meter          E    =           
0010269
 Z    =       -5002278
91                 I    =           51
57902
 XDOT =      -7026
460503                 Wp   =           92
56918
 YDOT =      -2473
946276  meter/sec      RA   =          187
64733  deg
 ZDOT =       1912
406180                 TA   =          195
91954
                                          MA   =          195
95184
                                          Ha   =            191
931  n
mi
                                          Hp   =            186
942

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       -8674372
06                 X    =        -2660248
50
 Y    =       11969636
42  feet           Y    =         3618688
24  meter
 Z    =      -16411676
22                 Z    =        -5015162
45
 XDOT =     -23052
691940                 XDOT =       -7007
564270
 YDOT =      -8116
621642  feet/sec       YDOT =       -2552
414673  meter/sec
 ZDOT =       6274
298490                 ZDOT =        1878
317631

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =        6761504
31                 X    =         2060906
51
 Y    =      -13083465
47  feet           Y    =        -3987840
27  meter
 Z    =      -16461015
57                 Z    =        -5017317
55
 XDOT =      23064
385004                 XDOT =        7030
024549
 YDOT =       4203
373802  feet/sec       YDOT =        1281
188335  meter/sec
 ZDOT =       6142
536021                 ZDOT =        1872
244979


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08205
69958554  
00020000  00000-0  20000-3 0  9083
2 25544  51
6400 188
6045 0003796 317
7378  42
3492 15
72462572 34283


Satellite: ISS
Catalog Number: 25544
Epoch time:      08205
69958554   =   yrday
fracday
Element set:     908
Inclination:       51
6400  deg
RA of node:       188
6045  deg
Eccentricity:     
0003796     
Arg of perigee:   317
7378  deg
Mean anomaly:      42
3492  deg
Mean motion:   15
72462572  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3428
Checksum:              318


Coasting Arc #10 (Orbit 3443)
---------------------------------------

Vector Time (GMT): 2008/206/16:29:06
528
Vector Time (MET): N/A
Weight (LBS)     : 660953
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        6503680
56                 A    =         6735965
57  meter
 Y    =        1251715
57  meter          E    =           
0005560
 Z    =       -1214738
07                 I    =           51
64318
 XDOT =      -1972
121100                 Wp   =          144
11490
 YDOT =       4564
586973  meter/sec      RA   =          182
54842  deg
 ZDOT =      -5873
101025                 TA   =           49
18552
                                          MA   =           49
13731
                                          Ha   =            192
032  n
mi
                                          Hp   =            186
986

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =       21337534
64                 X    =         6495101
26
 Y    =        4106678
37  feet           Y    =         1324395
58  meter
 Z    =       -3985361
11                 Z    =        -1183164
03
 XDOT =      -6470
213584                 XDOT =       -1994
486101
 YDOT =      14975
679044  feet/sec       YDOT =        4542
408995  meter/sec
 ZDOT =     -19268
704151                 ZDOT =       -5882
735523

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =      -21742750
07                 X    =        -6627190
22
 Y    =        -604272
61  feet           Y    =         -184182
29  meter
 Z    =       -3863414
16                 Z    =        -1177568
64
 XDOT =       3814
752920                 XDOT =        1162
736690
 YDOT =     -14220
437900  feet/sec       YDOT =       -4334
389472  meter/sec
 ZDOT =     -19305
420017                 ZDOT =       -5884
292021


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08206
71640862  
00020000  00000-0  20000-3 0  9098
2 25544  51
6404 183
3944 0003760 320
5110  39
5778 15
72457947 34447


Satellite: ISS
Catalog Number: 25544
Epoch time:      08206
71640862   =   yrday
fracday
Element set:     909
Inclination:       51
6404  deg
RA of node:       183
3944  deg
Eccentricity:     
0003760     
Arg of perigee:   320
5110  deg
Mean anomaly:      39
5778  deg
Mean motion:   15
72457947  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3444
Checksum:              297


Coasting Arc #11 (Orbit 3459)
---------------------------------------

Vector Time (GMT): 2008/207/16:29:06
528
Vector Time (MET): N/A
Weight (LBS)     : 660953
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =         752425
35                 A    =         6724513
83  meter
 Y    =       -4171137
30  meter          E    =           
0004779
 Z    =        5220716
44                 I    =           51
63423
 XDOT =       7646
148201                 Wp   =            6
25592
 YDOT =        320
316087  meter/sec      RA   =          177
40621  deg
 ZDOT =       -841
329497                 TA   =           91
78308
                                          MA   =           91
72834
                                          Ha   =            191
981  n
mi
                                          Hp   =            186
821

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        2468587
09                 X    =          773650
46
 Y    =      -13684833
67  feet           Y    =        -4162605
09  meter
 Z    =       17128334
79                 Z    =         5224422
87
 XDOT =      25085
788060                 XDOT =        7646
085120
 YDOT =       1050
905798  feet/sec       YDOT =         405
819438  meter/sec
 ZDOT =      -2760
267379                 ZDOT =        -804
184644

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =         108692
74                 X    =           33129
55
 Y    =       13888155
99  feet           Y    =         4233109
95  meter
 Z    =       17142221
46                 Z    =         5224949
10
 XDOT =     -23873
218152                 XDOT =       -7276
556893
 YDOT =       3436
069216  feet/sec       YDOT =        1047
313897  meter/sec
 ZDOT =      -2616
908319                 ZDOT =        -797
633656


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08207
73322202  
00020000  00000-0  20000-3 0  9108
2 25544  51
6400 178
1844 0003925 324
1468  35
9430 15
72526535 34606


Satellite: ISS
Catalog Number: 25544
Epoch time:      08207
73322202   =   yrday
fracday
Element set:     910
Inclination:       51
6400  deg
RA of node:       178
1844  deg
Eccentricity:     
0003925     
Arg of perigee:   324
1468  deg
Mean anomaly:      35
9430  deg
Mean motion:   15
72526535  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3460
Checksum:              266


Coasting Arc #12 (Orbit 3475)
---------------------------------------

Vector Time (GMT): 2008/208/16:29:06
528
Vector Time (MET): N/A
Weight (LBS)     : 660953
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =       -6686385
49                 A    =         6736455
90  meter
 Y    =         706443
85  meter          E    =           
0013998
 Z    =         248974
56                 I    =           51
70347
 XDOT =       -274
302810                 Wp   =           31
75519
 YDOT =      -4773
840387  meter/sec      RA   =          172
29323  deg
 ZDOT =       6037
460244                 TA   =          330
94735
                                          MA   =          331
02518
                                          Ha   =            192
193  n
mi
                                          Hp   =            186
765

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =      -21936960
28                 X    =        -6694997
59
 Y    =        2317729
16  feet           Y    =          631624
66  meter
 Z    =         816845
67                 Z    =          216471
27
 XDOT =       -899
943604                 XDOT =        -250
229466
 YDOT =     -15662
205995  feet/sec       YDOT =       -4776
773956  meter/sec
 ZDOT =      19807
940433                 ZDOT =        6036
185555

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       21066115
62                 X    =         6420952
04
 Y    =       -6558197
35  feet           Y    =        -1998938
55  meter
 Z    =         691485
38                 Z    =          210764
74
 XDOT =       3574
146712                 XDOT =        1089
399918
 YDOT =      13626
496903  feet/sec       YDOT =        4153
356256  meter/sec
 ZDOT =      19802
550427                 ZDOT =        6035
817370


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08208
75003056  
00020000  00000-0  20000-3 0  9115
2 25544  51
6403 172
9739 0003938 329
4408  30
6525 15
72494576 34763


Satellite: ISS
Catalog Number: 25544
Epoch time:      08208
75003056   =   yrday
fracday
Element set:     911
Inclination:       51
6403  deg
RA of node:       172
9739  deg
Eccentricity:     
0003938     
Arg of perigee:   329
4408  deg
Mean anomaly:      30
6525  deg
Mean motion:   15
72494576  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3476
Checksum:              300


Coasting Arc #13 (Orbit 3490)
---------------------------------------

Vector Time (GMT): 2008/209/16:29:06
528
Vector Time (MET): N/A
Weight (LBS)     : 660953
8

          M50 Cartesian                         M50 Keplerian  
-----------------------------------       --------------------------------
 X    =        1203981
86                 A    =         6724322
21  meter
 Y    =        4002745
13  meter          E    =           
0013801
 Z    =       -5278811
91                 I    =           51
69202
 XDOT =      -7445
943372                 Wp   =           73
03773
 YDOT =       1900
766488  meter/sec      RA   =          167
17330  deg
 ZDOT =       -253
568795                 TA   =          194
53370
                                          MA   =          194
57342
                                          Ha   =            192
242  n
mi
                                          Hp   =            186
623

          M50 Cartesian                         J2K Cartesian  
-----------------------------------       --------------------------------
 X    =        3950071
73                 X    =         1184776
49
 Y    =       13132365
91  feet           Y    =         4016102
16  meter
 Z    =      -17318936
71                 Z    =        -5273009
02
 XDOT =     -24428
948071                 XDOT =       -7465
412858
 YDOT =       6236
110524  feet/sec       YDOT =        1817
392854  meter/sec
 ZDOT =       -831
918619                 ZDOT =        -289
788105

          TDR Cartesian                         TDR Cartesian  
-----------------------------------       --------------------------------
 X    =       -6742685
54                 X    =        -2055170
55
 Y    =      -11974434
54  feet           Y    =        -3649807
65  meter
 Z    =      -17296149
25                 Z    =        -5271866
29
 XDOT =      21671
779940                 XDOT =        6605
558526
 YDOT =     -10783
738698  feet/sec       YDOT =       -3286
883555  meter/sec
 ZDOT =       -971
520187                 ZDOT =        -296
119353


The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time


TWO LINE MEAN ELEMENT SET

ISS
1 25544U 98067A   08209
70327917  
00020000  00000-0  20000-3 0  9127
2 25544  51
6405 168
0893 0003952 332
7894  27
3061 15
72531554 34917


Satellite: ISS
Catalog Number: 25544
Epoch time:      08209
70327917   =   yrday
fracday
Element set:     912
Inclination:       51
6405  deg
RA of node:       168
0893  deg
Eccentricity:     
0003952     
Arg of perigee:   332
7894  deg
Mean anomaly:      27
3061  deg
Mean motion:   15
72531554  rev/day
Decay rate:    2
00000E-04  rev/day^2
Epoch rev:            3491
Checksum:              296

INTERNATIONAL SPACE STATION ORBITAL DATA:

The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:

NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission

By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command

   David Cottle
   Director Of Engineering
   IDB Communications

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